发明名称 |
Shrouded turbofan bleed duct |
摘要 |
A bleed duct (42) is configured for bleeding fan air from the fan bypass duct (32) in a turbofan aircraft engine (10). The bleed duct (42) includes a tubular conduit (48) having an inlet (50) and outlet (52) at opposite ends. The conduit (48) is configured in flow area for recovering pressure from speeding fan air bled therethrough. A shroud (60,68,70,72,74) extends forwardly from the duct inlet (50) for suppressing dynamic pressure oscillations inside the conduit (48) without degrading the pressure recovery. |
申请公布号 |
EP1795708(A3) |
申请公布日期 |
2012.12.05 |
申请号 |
EP20060125745 |
申请日期 |
2006.12.08 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
KRAFT, ROBERT EUGENE;GIBBENS, NELSON DIRK;HETICO, ROLF ROBERT;GROLL, WILLIAM CHARLES;BAILEY, WILLIAM ANDREW;STOKER, JAMES EDWARD |
分类号 |
F01D9/06;F02C6/08;F02C7/32;F02C9/18;F02K3/06 |
主分类号 |
F01D9/06 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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